Code of Federal Regulations · Section

§ 29.181 — Dynamic Stability: Category A Rotorcraft

14 C.F.R. § 29.181

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Any short-period oscillation occurring at any speed from VY to VNE must be positively damped with the primary flight controls free and in a fixed position.

14 C.F.R. § 29.177 14 C.F.R. § 29.231

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